CA2474327A1 - Seal assembly for a pressurized fuel feed system for an internal combustion engine - Google Patents

Seal assembly for a pressurized fuel feed system for an internal combustion engine Download PDF

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Publication number
CA2474327A1
CA2474327A1 CA002474327A CA2474327A CA2474327A1 CA 2474327 A1 CA2474327 A1 CA 2474327A1 CA 002474327 A CA002474327 A CA 002474327A CA 2474327 A CA2474327 A CA 2474327A CA 2474327 A1 CA2474327 A1 CA 2474327A1
Authority
CA
Canada
Prior art keywords
sealing surface
ring
throttle
internal combustion
fluid
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002474327A
Other languages
French (fr)
Other versions
CA2474327C (en
Inventor
Gene Mcclendon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cameron International Corp
Original Assignee
Cooper Cameron Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Cooper Cameron Corp filed Critical Cooper Cameron Corp
Publication of CA2474327A1 publication Critical patent/CA2474327A1/en
Application granted granted Critical
Publication of CA2474327C publication Critical patent/CA2474327C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/021—Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/028—Sealings between relatively-stationary surfaces with elastic packing the packing being mechanically expanded against the sealing surface
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/08—Throttle valves specially adapted therefor; Arrangements of such valves in conduits
    • F02D9/10—Throttle valves specially adapted therefor; Arrangements of such valves in conduits having pivotally-mounted flaps
    • F02D9/1035—Details of the valve housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/04—Gas-air mixing apparatus
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0203—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels characterised by the type of gaseous fuel
    • F02M21/0215—Mixtures of gaseous fuels; Natural gas; Biogas; Mine gas; Landfill gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0296—Manufacturing or assembly; Materials, e.g. coatings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/30—Use of alternative fuels, e.g. biofuels

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Gasket Seals (AREA)

Abstract

A sealing assembly for a pressurized fuel feed system for an internal combustion engine is disclosed. The seal assembly comprises providing a fuel conduit having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction with a first sealing surface disposed on the fuel conduit. A second sealing surface engages with the first sealing surface, such as to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage. The said first and second sealing surfaces are substantially perpendicular to the general fluid-flow direction.
An o-ring is disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection. Preferably the o-ring is subjected to a squeeze of at least 40%, more preferably 50%, when the first and second sealing surfaces are coupled together. The sealing arrangement is most advantageously applied to throttle assemblies and the like, in particular for use with low-speed, gaseous fueled engines.

Claims (34)

1. A fuel supply system for an internal combustion comprising:
a fuel conduit having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction;
a first sealing surface disposed on the fuel conduit;
a second sealing surface engaged with the first sealing surface, such as to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage;
said first and second sealing surfaces are substantially perpendicular to the general fluid-flow direction;
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection.
2. The fuel supply system as claimed in claim 1, wherein the o-ring extends around the fuel conduit.
3. The fuel supply system as claimed in claim 1, wherein the fuel conduit is a throttle body.
4. The fuel supply system as claimed in claim 3, wherein the second sealing surface is formed on cover plate mounted over an opening in the throttle body.
5. The fuel supply system as claimed in claim 3, further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
6. The fuel supply system as claimed in claim 1, wherein the first sealing surface is formed on a flange extending from the fuel conduit.
7. The fuel supply system as claimed in claim 1, wherein the o-ring is located in a groove.
8. The fuel supply system as claimed in claim 7, wherein the groove is formed in the first sealing surface.
9. The fuel supply system as claimed in claim 1, wherein the o-ring is subjected to a squeeze of greater than 30%.
10. The fuel supply system as claimed in claim 9, wherein the o-ring is subjected to a squeeze of at least 40%.
11. The fuel supply system as claimed in claim 10, wherein the o-ring is subjected to a squeeze of at least 50%.
12. A throttle for a fuel supply system of an internal combustion engine, the fuel supply system supplying a pressurized normally gaseous fuel to the engine, the throttle comprising:
a throttle body having a fluid flow passage therethrough for conveyance of a pressurized fuel-containing gas in a general fluid-flow direction;
a first sealing surface disposed on the throttle body;
a second sealing surface engaged with the first sealing surface, such as to provide a fluid-tight connection preventing pressurized gas from leaving the fluid flow passage;

an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection.
13. The throttle as claimed in claim 12, wherein the first and second sealing surfaces extend substantially perpendicular to the general fluid-flow direction.
14. The throttle as claimed in claim 13, wherein the o-ring extends around the fluid flow passage.
15. The throttle as claimed in claim 12, wherein the second sealing surface is formed on cover plate mounted over an opening in the throttle body.
16. The throttle as claimed in claim 12, further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
17. The throttle as claimed in claim 12, wherein the first sealing surface is formed on a flange extending from the throttle body.
18. The throttle as claimed in claim 12, wherein the o-ring is located in a groove.
19. The throttle as claimed in claim 18, wherein the groove is formed in the first sealing surface.
20. The throttle as claimed in claim 12, wherein the o-ring is subjected to a squeeze of greater than 30%.
21. The throttle as claimed in claim 20, wherein the o-ring is subjected to a squeeze of at least 40%.
22. The throttle as claimed in claim 21, wherein the o-ring is subjected to a squeeze of at least 50%.
23. A low speed, pressurized gaseous fuel internal combustion engine comprising:
a fuel feed system for supplying pressurized gaseous fuel to an inlet of the internal combustion engine;
the fuel feed system comprising a throttle for regulating the flow of pressurized gaseous fuel to the internal combustion engine;
the throttle comprising a throttle body having a fluid flow passage therethrough for conveyance of the pressurized gaseous fuel in a general fluid-flow direction;
a first sealing surface disposed on the throttle body;
a second sealing surface engaged with the first sealing surface, such as to provide a fluid-tight connection preventing pressurized gaseous fuel from leaving the fluid flow passage;
an o-ring disposed between the first sealing surface and second sealing surface, the o-ring being compressed by the first and second sealing surfaces to form said fluid-tight connection.
24. The internal combustion engine as claimed in claim 23, wherein the first and second sealing surfaces extend substantially perpendicular to the general fluid-flow direction.
25. The internal combustion engine as claimed in claim 24, wherein the o-ring extends around the fluid flow passage.
26. The internal combustion engine as claimed in claim 23, wherein the second sealing surface is formed on cover plate mounted over an opening in the throttle body.
27. The internal combustion engine as claimed in claim 23, further comprising an actuator for the throttle, wherein the second sealing surface is formed on the actuator.
28. The internal combustion engine as claimed in claim 23, wherein the first sealing surface is formed on a flange extending from the throttle body.
29. The internal combustion engine as claimed in claim 23, wherein the o-ring is located in a groove.
30. The internal combustion engine as claimed in claim 29, wherein the groove is formed in the first sealing surface.
31. The internal combustion engine as claimed in claim 23, wherein the o-ring is subjected to a squeeze of greater than 30%.
32. The internal combustion engine as claimed in claim 31, wherein the o-ring is subjected to a squeeze of at least 40%.
33. The internal combustion engine as claimed in claim 32, wherein the o-ring is subjected to a squeeze of at least 50%.
34. The internal combustion engine as claimed in claim 23, wherein the o-ring provides a seal under an operating pressure for the pressurized gaseous fuel of up to 100 psi.
CA2474327A 2003-08-12 2004-07-15 Seal assembly for a pressurized fuel feed system for an internal combustion engine Expired - Fee Related CA2474327C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/639,540 US8037871B2 (en) 2003-08-12 2003-08-12 Seal assembly for a pressurized fuel feed system for an internal combustion engine
US10/639,540 2003-08-12

Publications (2)

Publication Number Publication Date
CA2474327A1 true CA2474327A1 (en) 2005-02-12
CA2474327C CA2474327C (en) 2011-10-04

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CA2474327A Expired - Fee Related CA2474327C (en) 2003-08-12 2004-07-15 Seal assembly for a pressurized fuel feed system for an internal combustion engine

Country Status (3)

Country Link
US (2) US8037871B2 (en)
CA (1) CA2474327C (en)
MX (1) MXPA04007436A (en)

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Also Published As

Publication number Publication date
CA2474327C (en) 2011-10-04
MXPA04007436A (en) 2005-02-17
US20120073544A1 (en) 2012-03-29
US8813727B2 (en) 2014-08-26
US8037871B2 (en) 2011-10-18
US20050034705A1 (en) 2005-02-17

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Effective date: 20160715